AD/GROB 115/4 - Firewall Bonding Lead

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B10323 In force Legislative Instrument

Legislation content

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Grob G115 Series Aeroplanes

 

AD/GROB 115/4 Firewall Bonding Lead 11/91

Applicability: All G115A series aircraft S/No 8091 through 8109 inclusive, except S/Nos 8097, 8100 and 8102.

 

Requirement: Action in accordance with the technical requirements of GROB G115 Service Bulletin TM 1078-18.

 

Compliance: Within 25 hours Time in Service after 14 November 1991.

 

Background: Grob have advised that during engine start, there is a possibility that a high resistance may occur at the bonding lead assembly mounted at the firewall.

 

This may cause a reverse current to occur which may damage wiring and other aircraft components. To prevent this, the existing bonding bolt plate must be replaced with a modified bonding bolt plate (P/No 115-9006).

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Interactions

Authorises

All Versions

Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.